Rapid acting laser q-switch



March 18, 1969 J. F. FORKNER RAPID ACTING LASER Q-SWIICH Sheet Filed Feb. 24,` 1964 March 18, 1969 J. F. FORKNER RAPID ACTING LASER Q-SWITCH sheet-M4 Filed Feb.v 24, 1964 RAY me MMM/zml Q 24a' l AMA/7 March 18,51969 J. F. FQRKNER I 3,4-'.40'3` RAPID ACTING LASER Q-SWITCH Filed Feb. 24, 1964 sheet 3 of 4 t7 armen/W6;

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March i, W6 J.' F, FORKNER 3,434,03

RAPID ACTING LASER Q-SWITCH Filed Feb, 24, 1964v sheet 4 'or 4 INVENTOR. d//A/ FORK/Vf?? nited States Patent 3,434,073 Patented Mar. 18, i969 3 Claims ABSTRACT F THE DISCLOSURE A relatively high-speed optical shutter for use in the optical system of a laser for greatly increasing its peak power output. In one aspect, the optical shutter comprises a's'ystem of prisms arranged to cause multiple impingement of the internal laser beam on a rotatable mirror, whereby to -multiply the angular sweep rate of the laser beam as it is reflected back into the laser medium. In another aspect, the optical shutter includes a telescope arranged to increase the apparent rotational speed of the mirror, and hence the angular sweep rate of the beam, by magnifying the width of the beam reflected back into the laser medium.

This invention relates to laser apparatus, and more particularly to improvements in so-called Q-spoiling devices of giant-pulse lasers.

In one known form of laser the working element is a single crystal of pink ruby in the form of a cylindrical rod, of for example about one-half centimeter in diameter and 4 centimeters in length, and having flat end faces that are plane to a high degree of accuracy. The ruby rod is disposed between two parallel reflecting surfaces, at least one of which may be formed on the end of the rod. One surface is completely reflecting and the other surface is only partially reflecting. The ruby rod is irradiated, or pumped, laterally of its axis by light-from a high intensity light source, such as a flash lamp, operated usually for a few milliseconds at a time with an input of relatively high value. A fraction of the energy emitted by the flash lamp is absorbed by the ruby crystal. When the energy absorbed from the exciting irradiation exceeds a certain threshold, and a very short time after the start ofv irradiation, coherent radiation emerges in a narrow` beam through the partially reflecting surface which forms one end of the resonant optical system of the laser.

The intensity of the laser beam varies irregularly, it having been observed that the time delays between the start of excitation and the onset of coherent oscillations are not uniform in spite of efforts to keep all experimental variables under contr'pldOnce coherent light appears, its intensity will vary greatly and irregularly with spikes, or pulsations, of durations of about 1 rnicrosecond.

It is possible to overcome the aforementioned irregularities and to increase the peak intensity of the output pulse by temporarily lowering or spoiling the Q of the optical system of the laser. By this so-called Q-spoiling the laser crystal can be irradiated, or pumped, past the normal threshold value at which it begins to emit coherent radiation. After the pumping irradiation has attained a condition of saturation, the optical characteristics of the system are -again modified by suddenly raising or, unspoiling, the Q, with the result that a relatively large burst of radiant energy is emitted by the crystal. For example, a conventional laser system which would normally produce a series of spikes having a peak power of 50 kilowatts when operated in the manner just described may achieve a peak output of 5 megawatts. Systems of this type are known in the art as giant-pulse laser systems.

Q-spoiling in the optical system of the laser normally is accomplished by means of a light shutter placed between the ruby rod -and one of the reflecting surfaces, or

to flash so that the pumping begins just before the shutter,

is opened, or just before the rotating reflective mirror or prism is brought into optical alignment with the end of the laser crystal. The -amplitude of the pulse produced is dependent to a large extent upon the rapidity with which the shutter is opened or the reflective surface is brought into optical alignment. A

It is an object of this invention to provide, in a Q- spoiling system as described, optical means operative greatly to multiply the effective rotational rate of the reflective means.

It is a further objective of the invention to provide, in a giant pulse laser apparatus, optical means to increase the effective operating speed of the shutter.

The invention contemplates, in one form thereof, that the reflective means comprises a rotating-mirror shutter considerably larger in diameter than the cross-section of a ruby crystal, and interposing a telescope between the rotating mirror and the end of the ruby crystal. In this embodiment the effective rotational rate of the mirror is proportional to the product of its actual rotational rate and the magnification of the telescope.

The invention further contemplates that the laser Q- spoiler may comprise a plurality of prisms, one of which is rotated. The optical path between the two reflecting surfaces of the laser optical system is folded so that energy emitted by the laser rod is caused to be reflected by a face of the rot-ating prism a plurality of times. This may be achieved by means of suitably positioned, stationary reflectors, such for example, as roof prisms. The multiple reflections from the rotating prism have the effect of multiplying the apparent speed of rotation of the rotating prisms, Thus an increase in the apparent speed of the Q- spoiling action is achieved advantageously without an increase inthe prism rotation rate,

Still further, it is contemplated by the invention that the above-described telescope and rotating prism arrange-- ments may fbe combined to achieve still faster, high fre-` quency shutter operation.

The invention may therefore be briefly summarized as* comprising a combination of: a working element capable of laser action; reflective shutter means disposed and adapted to reflect radiation emitted by said element back into the latter; means for establishing the operating speed of said shutter means; and means operable optically to modify the effective operating speed of the shutter.

For a more complete understanding of the invention, reference may be had to the following detailed description, taken in light of the accompanying drawings in which:

FIGURE l is a vsomewhat diagrammatic showing, partly in perspective, of giant-pulse laser apparatus embodying the invention;

FIGURE 2 is a perspective view', on a reduced scale, of a portion of the apparatus illustrated in FIGURE l, and in which one of the elements has been modified slightly;

FIGURE 3 is a plan view of the apparatus illustrated in FIGURE 2;

FIGURE 4 is a somewhat diagrammatic showing of apparatus illustrated in FIGURES 1 to 3, and demontratiing optical principles upon which the invention is ase FIGURE 5 is a further diagrammatic showing of the optical principles of the invention;

FIGURE 6 is a view similar to FIGURE 2 and illustrating a modified embodiment of the invention;

FIGUR-E '7 is a view similar to FIGURE 6 and illustrating another modified embodiment of the invention;

FIGURE 8 is a view similar to FIGURES 6 and 7 and illustrating a further modified embodiment of the inven tion; and

FIGURES 9 through 12A comprise additional modified embodiments of the invention, in which different optical systems are utilized.

With more particular reference to FIGURE l, laser apparatus embodying the invention comprises a cylindrically formed crystal 10 of suitable material, for example pink ruby, having end faces 11 and 12 that are plane to a high degree of accuracy. End face 11 is provided with a partially reflective coating and face 12 has no reflective coating. A helically formed xenon llash tube 13 is coiled about crystal 10', and is energized by a suitable power supply 14 of known construction. A rotatable prism 15 drivingly coupled with a motor 16, and a lamp 17 disposed and adapted to emit a beam for sequential reflections by external faces of rotating prism 15 onto a detector 21. Rellections by rotating prism 15 of the light beam from lamp 17 -will reach detector 21 according to the sequential positional relationships of the outer reflective faces of the prism 15. Detector 21 is constructed and arranged to actuate a pulse generator 22 which in turn triggers power supply 14, as the face 18 of the rotatable prism reaches the position shown, in which position said face reflects the beam onto the detector.

As a practical matter, in view of the relatively high rotational rate of prism 15 and compared with the time required for flash lamp 13 to fire, a typical pulse rate is one per 10 seconds, as may be provided by an operator who actuates a trigger or push-button switch, such as is seen at 29, to fire the laser. The illustrated synchronizing system, upon actuating the trigger switch, operates to fire the prism 15 as rotated into beam reflecting position, or just prior to such optical alignment of prism 15 as to provide for return of the emitted beam to nonreflecting end 12 of laser rod 10.

The Q-spoiling means comprises stationary prisms 23 and 24 so optically positioned as respects one another and rotatable prism 15, as to provide the illustrated light paths to and from the light transmissive or non-rellective end face 12 of ruby crystal 10', in accordance with the directional arrows. It will be appreicated that the complete light paths exist only for the illustrated position of the vrotatable prism 15, just following energization of xenon lamp 13. The several prisms therefore comprise the fully reflective means for end face 12 of the laser rod, and as will be described in what follows, rotation of prism 15 alternatively spoils and restores the Q of the laser optical system.

In FIGURE 1, locations of all rays of light entering or leaving the prisms are designated by the letter A. The light rays leaving the end 12 of rod 10iI are polarized in a vertical plane, and the prism dimensions and angles are selected so that such rays enter and leave at the so-called Brewster angle at which no reflection losses occur for incident light polarized in the plane of incidence. The Brew ster angles are designated in FIGURE 3 by their actual values, and are based on materials having a refractive index of 1.52. However, it will be understood that these values are for illustrative purposes only, and materials having other refractive indices may be used.

All reflections inside the prisms are designated by the letter B and occur at less than the critical angle. Hence, these reflections are lossless, or totally internal. The only losses within the optical system comprising the shutter and reflector means are due to the prism material itself. These losses can be minimized substantially by selecting the proper material for the wave length ofthe light emitted by ruby crystal 10.

It will be noted that the difference between the apparatus illustrated in FIGURE 2 and the corresponding apparatus illustrated in FIGURE 1 is that the ruby rod or crystal 10 shown in FIGURE 2 has its non-reflective face 12a cut at the Brewster angle, whereas the corresponding Cil face 12 in FIGURE 1 is cut normal to the major axis of the rod. Also it will be noted in FIGURE 2 that the letters A and B have been replaced wiLh numerals 1 to 10 that correspond to the sequential paths of the light beam through'the prisms, as will be more fully discussed in what follows.

It can be shown, and as `will be more fully understood from the equivalent mirror systems illustrated in FIG- URES t` and 5, that upon rotation of prism 15 through a predetermined given angle, beams reflected, as at points B in this prism, will each be rotated or swept through twice the said given angle. It follows, therefore, that each reflected beam sweeps at double the rotational rate of the reflective" surface. Since there are four such rellections, the returning beam will sweep across the end of the laser rod at an angular speed eight times the rotational speed of prism 15.

While the light rays or beams in FIGURES 1 and 2 are shown as being spaced for the sake of clarity in tracing the path of the beam from and to the rod in restoration of reflection, or unspoiling of the Q, the corresponding rays are illustrated as coincident rays in FIGURE 3. Rays to either side thereof also have been included to indicate the limits of the lateral disposition of the rays.

With particular reference to FIGURE 2, andA assuming that xenon lamp 13 has just been fired to irradiate rod 10', an emitted beam leaving the end 12a of laser rod 10' will enter face 18 of rotating prism 15, thereafter to impinge upon rellection point 1 on face 20, from which the beam will be reflected to leave face 19 of the rotating prism. The beam will then enter the vertical face 25 of stationary roof prism 24 thereafter to impinge upon rellection point 2 which lies in the plane of the sloping face 26 of prism 24. The beam then will be deviated through a angle to impinge upon reflection point 3 on the lower sloping face 27 of prism 24, and at this point the `beam will ybe deviated again through a 90 angle to emerge from the vertical face 25 of prism 24 and will enter the vertical face 19 of rotating prism 15. The beam then will be deviated through a 90 angle (other angles of deviation could `be used provided that total internal reflection occurs at surface 20) by rellection at point 4 to emerge from the vertical face 18 of prism 15 and enter the vertical face 28 of prism 23. The beam is then turned by successive reflections at points 5 and 6 upon surfaces 30 and 29, respectively, to emerge from vertical face 28 of prism 23 and enter vertical face 18 of rotating prism 15. The beam then will be reflected at point 7 on face 20, emerge from vertical face 19 of prism 15, and enter vertical face 25 of prism 24 to be turned 180 by successive reflections from points 8 and 9 on faces 27 and 26, respectively. The reflected beam again will emerge from the vertical face 25 of prism 24 and enter vertical face 19 of prism 15, reflected at point 10 on face 20 to emerge from the other face 18 of prism 15 and return in a sweeping motion to end 12a of laser rod 10'. Shortly thereafter a giant pulse lbeam is emitted from partially reflective face 11, as indicated in FIGURE 1.

By virtue of the rotation of prism 15, the 'beam returned in restoration of reflection will have been deviated twice the angle through which the prism has turned for each of internal reflections 1, 4, 7, and 10 by face 20. Accordingly the sweep rate of the returning beam will be eight times the rotational rate of prism1v5, and substantially complete reflection will be achieved only for the very short period that the returning beam impinges on the laser rod. Importantly, the Q is restored with such rapidity as to produce a giant-pulse, the ideal condition for achieving a giant-pulse being the restoration of Q from zero to maximum in zero time. If the Q is restored with insufficient rapidity, no giant pulse will occur.

It will therefore be appreciated that the alternate spoiling and restoring of the optical path occurs more rapidly than with single mirror systems heretofore used. Also,

it will be appreciated that the rotational speed of the rotatable prism can Ibe further multiplied optically by inclusion of additional reflective prisms positioned to reflect the beam back into the rotating prism prior to return of the ybeam to the laser rod.

In the interest of further describing the invention and with reference to FIGURE 4, the prisms of the optical system illustrated in FIGURES 1, 2, and 3 have been replaced generally by mirrors bearing the same reference numerals as the corresponding prisms but with the suflix a applied.

To simplify the FIGURE 4 showing, the double reflection points of prisms 23 and 24 have been replaced with single reflection pointsfor example points 2 and 3 are combinedas point 2, 3, points 5 and 6 as point 5, 6, and points 8 and 9 as point S, 9.

The numbers 1 to 10 therefore correspond generally to the reflection points similarly vdesignated in FIGURES 2 and 3. In FIGURE 4 the mirror 15g" has been rotated through an angle and reflection points 1, 4, 7, and 10 have been taken at the rotated positions of the mirror a.

Maximum Q, or-substantially complete reflection, is obtained with reflection occurringwhile mirror 15a is in the illustrated non-rotated position. Points of reflection affording maximum Q are indicated by numerals 1" to 10, and by notation directed to mirror 24a. In the position of mirror 15a at which maximum Q occurs, the illustrated emitted ray is returned to the laser rod substantially along thesame path as it left. In terms of the reference numerals, the emitted ray` first is reflected at point 1" on mirror 15a, thence impinges at point 2", 3" on mirror 24a, and is reflected back onto .point.4 on mirror 15a from which it is reilectedonto point 5", 6".

The ray then is caused to follow the same path with reflections at point 7 on mirror 15a, point 8", 9" on mirror 24a, back to point 10 on mirror 15a for return to the laser rod along the line on which the ray was emitted. While points 1 and l have been illustrated as lbeing substantially coincident, it will be understood that the point 1 will have been displaced slightly due to rotation of mirror 15a.

With reference to FIGURE 5, mirror 24a has been vfolded about. the illustrated rotated 'position of mirror 15a;` In the resulting diagram, for each time the beam strikes the mirror 24a (at points 2, 3 and 8, 9) the beam is deviated four times the angle of rotation 5 of prism 15a. Since the-mirror 24a is struck twice-2, 3 essentially are the same points, as are 8, 9-the total deviation is eight times the angular rotation of the rotating mirror' 15a. Considered another way, it can be demonstrated, using the geometry of FIGURE 5, that since the normals to the mirrorthrough points 2, 3 andl 8, 9 are parallel, then the total deviation is the sum of fthe original angle of incidence (26) and the nal angle of reflection (66), i.e. 2+6=8, as indicated on the diagram.

Since the returning beam sweeps `at eight times the angular rotational rate of the prism 15, the effective shutter operation, in restoring-the reflecti occurs in a fraction of the time achieved with a simple rotating mirror optical system.

With reference to the modified embodiment of the invention illustrated in FIGURE 6, laser rod 31 has a partially reflective end face 32 and a substantially non-reective, light transmissive end face 33. Prism 34 is rotatable about its longitudinal axis, has the cross-section ofy a 45 x 45 x 90 triangle, land is in optical alignment with, laser rod,31, and also with a stationary 45 x 45 x 90"y roof prism 35', and a like but smaller, stationary roof prism 36. In the illustrated positionof the rotatable prism, and for the sake of convenience, the ray of light emitted from face 33 of laser rod 31, immediately following irradiation of the same, is shown as returning along apath parallel to the path along which it is emitted in restoring theV Q of the system. The light ray will travel from rod 31 for multiple reflections by the prisms 34,' 35, and 36,

returning to the rod 31 will have a sweep rate eight times l the rotationalangular velocity of prism 34.

In FIGURE 7 there is illustrated a modification of the apparatus shown in FIGURE 6, the reflecting faces of the rotatingprism 40 being doubled as compared with prism 34 of FIGURE 6, and the number of roof prisms being increased to four, as seen at 41, 42, 43 and 44. There are eight reflections by the rotating prism of this system to l make the sweep rate of the emitted ray of light 16 times the prism angular velocity.

With more particular reference to FIGURE 7, each of prisms 41, 43, and 44 has the same configuration as prisms 35 and.36, for example, in that their roof surface portions lie iinplanes disposed at right angles to one another. The rotating prism 40 comprises two rotatably mounted pairs of 45 x 45 x 90 cross-sectional prisms 40a, 40b, 40C and 40d with hypotenuse faces spaced ap- A proximately .O05 in. apart. The mating hypotenuse faces of one pair of prisms (40a and 40b') are disposed at a right angle with respect to the mating faces of the other pair (40e and 40d).

In the interest of clarity, the rays entering and leaving l the sever-a1 prisms are illustrated as travelling along the same light paths, and will be traced by means of numbers 'applied to the reflection points. Starting with the ray as it leaves the laser rod following irradiation, it will first impinge a 101 the reflective face of prism 40a to be reflected upward for successive reflections at 102 and 103 i by sloping faces of roof prism 41. The ray leaves prismVv --f -41 to impinge at 104 upon the reflective face of prism 40C for successive reflections horizontally at 105 and 106 by i sloping faces of roof prism 42. The ray then enters prismiV 40b to be reflected at 107 on its reflective face downwardly-"if ing considered as coincident, points 111 and 112 also are-i coincident, `and the ray can be described as returning to:

the laser rod from point 112 by successive return re-` flections at points 110, 109, 108, 107, 106, 105, 104, 103;' 102, 101.

Whereas the embodiment illustrated in FIGURE 6 restores reflection to the system, or unspoils the Q, substantially eightjfimes faster `than a simple rotating mirror, theA embodiment illustrated in FIGURE 7 achieves Q restorations substantially sixteen times faster than does a simple rotating mirror.

The lapparatus illustrated in FIGURE 8 is similar to that shown in FIGURE 6, with .the exception thati` the prisms are so shaped and disposed that;-the angle Ai: at which the light enters a prism-each identified by the same reference numeral as thelcorrespondin'g prism in FIG- IURE 6, with the suflix a`is thehBrewster angle for the prism material. Therefore, no reflection losses occur at external surfaces of the prisms for light polarization in the vertical plane, as is'the case with the light'beam leaving the laser rod. The internal angles of reflection B' are greater than the critical angle for the prism material and hence total reflection occurs in the rotating prism 34a. The r`eflection angles B' in the two stationary prisms'35a -and 36a of the same material also are total reflections. As is the case with apparatus shown in FIGURE 6, this arrangement produces an angular sweep of the energy returning to the laser rod at a rate eight times the rotationalrate of the` rotating prism, and is thus substantially four times as rapid in sweeping the beam as is a simple mirror.

Turning now to the modified embodiment of the invention illustrated in FIGURE 9, a laser rod 51 having partially reflecting face 52 and a non-reflective face 53 is optically aligned with a rotatable plane mirror 54. The optical equivalent of a telescope is interposed between the nonreflective end 53 of laser rod 51 and the mirror 54, the telescope comprising a plano-convex eyepiece lens 55 and a like objective lens 56, each arranged as shown. Mirror S4 and objective lens l56 are of the same diameter, larger than the cross-sectional area of laser rod end 53.

The paths of light rays emitted from and reflected onto non-reflecting end 53 of the rod 51 are indicated for convenience as travelling the same paths in either direction, and under condition of maximum reflection. The path of the giant pulse beam is indicated by arrows emanating from the partially reflecting face 52. While means for irradiating rod 51 has not been illustrated, it `will be appreciated that an arrangement similar to the one illustrated in FIGURE 1 may be utilized.

The gain of the telescope in FIGURE 9 effectively multiplies the -rotational rate of the mirror inasmuch as the beam -width emitted by end face 53 is magnified to the width of mirror 54 for a given rotational rate of the mirror. It follows, therefore, that if a wider reflected beam is swept at the angular rotational rate afforded by the rotating mirror, a resultant increase in beam velocity across the end 53 of rod 51 is achieved. For example, if mirror 54 rotates at 20,000 r.p.m., a telescope having a gain of has the effect of a smaller diameter mirror rotating at 5 times 20,000 r.p.m., or 100,000 r.p.m.

This principle of shutter speed magnification may be set forth as follows, using exemplary values as tabul-ated:

Pulse duration IO see. are (2) (5) 400 r.p.s. 360 -eissxaeoo See. arc/degree Pulse duration (time) seconds 2 l0g The factor (2) in the denominator represents the increase in sweep rate due to rotation of mirror 54.

In FIGURE 10, the embodiment illustrated in FIG- URE 9 has been modified substantially by making the non-reflective end of a laser rod `61 into a convex surface 62 and making the non-reflective surface of the rotatable mirror 63 convex as shown. This arrangement achieves the same magnification of the rotational speed of the mirror as does the embodiment shown in FIGU-RE 9, since the reflected beam width is again increased to that of the rotating mirror 63.

In the apparatus of both FIGURES 9 and 10 the beams include crossover points which can produce an energy concentration sufficient to ionize air in the region thereof. This latter problem, should it arise, can be overcome by the lens arrangement illustrated in FIGURE lll, in which the non-reflective end 67 of the laser rod 66 is made concave, and the rotatable mirror 68 is the same as the mirror 63 of FIGURE 10. The concavely curved surface of laser rod 66 serves as a negative lens, and in combination with curved rotatable mirror 68 comprises a Galilean telescope.

The rotatable mirror of FIGURE 1\1 can be also modified, if desired, to take the concave form 68a shown in FIGURE lla, in which the concave surface in made re`y .tlective.

Still further ,mpdifiegl apparatus embodying the inven- 8 tion is illustrated in perspective in FIGURE l2 and is similar to that illustrated in FIGURE lla. The primary difference is that the laser rod 71 is rectangular in cross section and vits concave, non-reflective end 72 projects rays onto a similarly rectangular concave reflective face of a rotatable mirror 7-3. In this rectangular arrangement each of the curved surfaces is cylindrical, and magnification is normal to the axis of rotation of the mirror 73. An advantage of this arrangement is that the mass of the rotating mirror is less than that of one with a generally spherical reflective surface, as in the previous example.

In FIGURE 12A, the rotatable mirror of FIGURE l2 has been replaced with a rotatable roof prism 73a provided with a convex face disposed for alignment with the concave face of the laser rod once for each revolution of the prism, and the light paths again are indicated by means of arrows.

In any of the embodiments illustrated in FIGURES 9 to 12A, the relatively large reflective surfaces reduce the power density at these surfaces, whereby there is less energy concentrated in the optical system. This characteristic permits operation at higher energy levels without damage to reflecting surface.

From the foregoing description it will be appreciated that the invention affords means for advantageously increasing the effective speed of a mechanical shutter for a laser device by optical means disposed in novel cooperative relationship with the shutter and the working e-lement of the device.

Iclaim:

1. In laser apparatus of the type including an active laser medium in the form of a rod having opposite end face portions, one face portion being partially light reflective and the other face portion being substantially totally light transmissive, means for pumping said laser medium to effect emission of a light beam from said other face portion, rotatable reflector means for reflecting said beam of light back onto said other face portion when said reflector means is in one of its rotated positions, and means for rotating said reflector means at a predetermined speed, the improvement comprising: optical means for reducing the duration of impingement of the reflected beam of light of said other face to a value less than the duration of impingement corresponding to the recited rotational speed of said reflector means, said optical means including fixed reflector means oriented with respect to said rotatable reflector means to effect a plurality of rellections of said beam of light by said rotatable reflector means prior to reflection of such beam by said rotatable reflector means onto said other face portion of said laser medium.

2. In laser apparatus according to claim 1, wherein said optical means comprises at least a first stationary roof prism and a second stationary roof prism, said first roof prism being positioned to receive light reected by said rotatable reflector means and effective to return such reflected light to said rotatable reflector means, said rotatable reflector means being oriented to reflect said light received from said first roof prism onto said second roof prism, said prisms in the recited reflector orientation beq ing effective to return said light to said rotatable reflector means for reflection onto said other face of said laser medium.

3. In laser apparatus according to claim 2, wherein said rotatable reflector means comprises a prism having external, light transmissive faces and an internal reflective face, said laser medium, said rotatable prism, said first roof prism, and said second roof prism being so constructed, and oriented relative to one another, that light enters and leaves external faces thereof at the Brewster angle with respect to said faces and in that ind ternal reflections of light are at angles greater than the critical angles of the respective recited elements of the apparatus.

(References on following page) Reereucesl Cied UNITED STATES PATENTS '10 FOREIGN PATENTS 3/'1962 Belgium.

OTHER REFERENCES JEWELL H. PBDERSEN, Primary Examiner,

E. BA'UER, Assistant Examiner.

Notice of Adverse Decision In Interference In Interference No. 97,162 involving Patent No. 3,434,073, J. F. Forkner, RAPID ACTING LASER Q-S\VITCH, nal judgment adverse to the patentee was rendered June 9, 1972, as t0 claims 1 and 2.

[Oficial Gazette November 21, 1.979.] 

